Casualties unknown

2011-06-18: Cessna 206 G (F-GDAA) — Conséquences et dommages, FR

Conséquences et dommages, FR

On June 18, 2011, a Cessna 206 G (registration F-GDAA) was involved in an aviation accident near Conséquences et dommages, FR. Investigators recorded the probable cause as: The engine failure was caused by a fatigue fracture of the number 4 connecting rod, likely initiated by machining scratches found in a bolt housing bore. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA).

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 1785058346Data APIEditorial standards

A Continental engine failure during initial climb resulted in an emergency landing at Saint-Etienne Bouthéon aerodrome.

What happened

On June 18, 2011, a Cessna 206 G, registration F-GDAA, was performing its ninth skydiving mission of the day from Saint-Etienne Bouthéon aerodrome. While climbing through an altitude between 4,000 and 5,000 feet, the pilot heard a loud noise coming from the engine, accompanied by significant vibrations and oil spraying onto the windshield.

Following established emergency procedures for an in-flight engine shutdown, the pilot executed a forced landing on the runway. The engine ceased operation during the landing roll.

The investigation

Investigators examined the Continental IO-520F engine and discovered two perforations in the upper crankcase near cylinders number 3 and 4. Detailed disassembly and inspection revealed that the engine failure was caused by the failure of the connecting rod for cylinder number 4 at its attachment point to the crankshaft.

Records showed the engine had been manufactured and installed on F-GDAA in 2004. Between February and April 2011, the engine underwent a major overhaul, which included a magnetic particle inspection (magnaflux) that failed to detect any fatigue cracks. At the time of the accident, the engine had accumulated 1,330 total operating hours, with only 63 hours and 29 cycles completed since the overhaul.

Probable cause

The engine failure was caused by a fatigue fracture of the number 4 connecting rod, likely initiated by machining scratches found in a bolt housing bore. The investigation could not determine if the crack was missed during the recent overhaul or if it developed during the 63 hours of operation following the overhaul.